View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 58838U 26145.42334030 +.00000000 +00000-0 -17972-5 0 00004
2 58838 53.1609 207.9572 0001071 89.8187 270.2937 15.30188867 07
| Epoch (UTC): | 25 May 2026 10:09:36 |
| Eccentricity: | 0.0001071 |
| inclination: | 53.1609° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.9572° |
| argument of perigee: | 89.8187° |
| revolutions per day: | 15.30188867 |
| mean anomaly at epoch: | 270.2937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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